about the course
registration & fee
Unsteady Simulations for Industrial Flows: Large Eddy Simulation (LES), hybrid LES-RANS, Detached Eddy Simulation (DES) and unsteady RANS
The traditional method for CFD in industry and universities is Reynolds-Averaged Navier-Stokes (RANS). It is a fast method and
mostly rather accurate. However, in flows involving large separation regions, wakes and transition it is inaccurate. The reason
is that all turbulence is modeled with a turbulence model. For predicting aeroacoustic, RANS is even more unreliable.
For these flow, Large-Eddy Simulation (LES) and Detached-Eddy Simulations (DES) is a suitable option although it is much more
expensive. But in many industries (automotive, aerospace, gas turbines, nuclear reactors, wind power) DES is used as an alternative to RANS.
In universities, extensive research has been carried out during the last decade(s) on LES and DES.
How to use an in-House Fortran source code
Unfortunately, most engineers and many researchers have limited knowledge of what a LES/DES CFD code is doing. The object of this
course is to close that knowledge gap. During the course, the participants will learn and work with an in-house LES/DES code called CALC-LES, written by the
lecturer. It is a finite volume code written in Fortran 77. It includes two zero-equation SGS models (Smagorinsky and WALE) and one
two-equation model (the PANS model).
The convective terms in the momentum equations are discretized using
Hybrid central/upwind is used for the k and eps equations. The Crank-Nicolson scheme is used for time discretization of all equations.
The numerical procedure is based on an implicit, fractional step technique with a
multigrid pressure Poisson solver  and a non-staggered grid arrangement.
CALC-LES is a single-block structured code. It is not
parallelized. However, it is very fast. The hump flow (see below), requires less than 4 seconds/time step on a standard PC. For a converged solutions,
7500+7500 time-steps are sufficient. The number of cells is 312x120x32.
The course includes lectures (12 hours) and workshops (12 hours) learning and using CALC-LES.
In the lectures we will address:
- finite volume discretization
- central differencing scheme
- hybrid central/upwind scheme
- Crank-Nicolson time discretization
- Rhie-Chow interpolation
- implicit fractional step method
- Smagorinsky model
- WALE model
- the k-eps DES model
- two-equation PANS model (k and epsilon)
- wall and periodic boundary conditions
- TDMA (tri-diagonal-matrix-algorithm) solver
- how to prescribe turbulent inlet boundary conditions
- how to generate inlet anisotropic synthetic turbulent fluctuations
In the workshops, the participants will use CALC-LES.
The participants will get the source code installed on their lap-top (participants must bring a lap-top!). It is recommended that the participants use Linux with the
GNU Fortran or Intel's ifort compiler
and have a simple plotting program, preferably Octave, installed. If participants use Windows or Mac, no support will be given for installing
Four test cases will be studied in detail:
- DNS and LES of fully developed channel flow [2-5]. Periodic boundary conditions in streamwise and
- LES of atmospheric boundary layer over a forest relevant to windpower engineering [10,11]. Periodic boundary conditions in streamwise and
spanwise directions. The figure show instantanoues streamwise velocity. The height of the forest (20m) is indicted by the green line.
A 384x192x96 mesh is used. The CPU time for one timestep on a standard desktop PC is 15 seconds.
- LES of the hill flow . Periodic boundary conditions in streamwise and
- DES of the hump flow . Synthetic inlet fluctuations at the inlet [7-9]. Periodic boundary conditions spanwise direction.
The object is that the participants should learn how a CFD code for LES/DES works. It will give them
increased knowledge, confidence and know-how when using commercial CFD codes.
The participants are expected to hold a MSC degree or PhD degree related to fluid mechanics. They are expected
to have at least a basic knowledge in LES and DES. Programming skills is also useful. The course is expected to be valuable also for researchers
with extensive knowledge in LES and/or DES. The participants may continue to use CALC-LES after the course, in their daily work and/or research. However, no support
will be given.
The lecturer at the course (both during lectures and workshops) will be Prof. Lars Davidson,
Chalmers University of Technology.
Note! Participants must bring a lap-top!
The course material is in English and the lectures will be given in English.
The course will be held 18-20 June 2018 in Göteborg at Waterfront Hotel and is organized by Flowsim AB.
Waterfront Hotel, Göteborg, Sweden.
Registration form should be submitted no later than May 18, 2018.
The price is 14,700 SEK (excl. VAT) which includes course material, lunches, coffee. No refunding after May 18. The number of participants is limited to 16.
DAY 1 (10.00 -- 19.00)
- General structure of CALC-LES
- Discretization in CALC-LES
- Compute geometrical quantities
- Fractional step method in CALC-LES
- Crank-Nicolson time discretization
- Studying Test Case 1 (channel flow)
- Studying Test Case 2 (atmospheric boundary layer)
DAY 2 (8.00 -- 17.00)
- Implicit Rhie-Chow interpolation in CALC-LES
- TDMA solver
- Implementation of Zero equation models
- Implementation of the PANS model in CALC-LES
- Studying Test Case 3 (hill flow)
DAY 3 (8.00 -- 17.00)
- How to implement a new turbulence model in CALC-LES
- Implementation of synthetic turbulence in CALC-LES
- How to generate anisotropic turbulent fluctuations in CALC-LES
- how to implement a k-eps DES model
- Pre-cursor RANS (using a 1D solver written in Matlab) as input to synthetic turbulence generator
- Studying Test Case 4 (hump flow)
QUESTiONS & FURTHER iNFORMATiON
- Lars Davidson
- tel. +46 (0) 730-791 161
- E-mail: firstname.lastname@example.org, email@example.com
- P. Emvin, The Full Multigrid Method Applied to Turbulent Flow in Ventilated
Enclosures Using Structured and Unstructured Grids. PhD thesis, Dept. of
Thermo and Fluid Dynamics, Chalmers University of Technology, Göteborg,
- L. Davidson, Large eddy simulations: how to evaluate resolution. International Journal of Heat and Fluid Flow, 30(5):1016-1025, 2009.
- L. Davidson, The PANS k-ε model in a zonal hybrid RANS-LES formulation. International Journal of Heat and Fluid Flow, 46:112-126, 2014.
- L. Davidson, Zonal PANS: evaluation of different treatments of the RANS-LES interface. Journal of Turbulence, 17(3):274-307, 2016.
- A. Altintas and L. Davidson, Direct numerical simulation analysis of spanwise oscillating lorentz force in turbulent channel flow at low Reynolds number. Acta Mechanica, pages 1-18, 2016.
- J. Ma, S.-H. Peng, L. Davidson, and F. Wang, A low Reynolds number variant of Partially-Averaged Navier-Stokes model for turbulence. International Journal of Heat and Fluid Flow, 32(3):652-669, 2011.10.1016/j.ijheatfluidflow.2011.02.001.
- L. Davidson, Using isotropic synthetic fluctuations as inlet boundary conditions for unsteady simulations. Advances and Applications in Fluid Mechanics, 1(1):1-35, 2007.
- L. Davidson and S.-H. Peng, Embedded large-eddy simulation using the partially averaged Navier-Stokes model. AIAA Journal, 51(5):1066-1079, 2013.
- L. Davidson, Two-equation hybrid RANS-LES models: A novel way to treat k and ω at inlets and at embedded interfaces. Journal of Turbulence, 18(4):291-315, 2017.
- B. Nebenfuhr, L. Davidson, Large-Eddy Simulation Study of Thermally Stratified Canopy Flow, Boundary-Layer Meteorology, Vol. 156, number 2 , pp. 253-276, 2015
- B. Nebenfuhr, L. Davidson, Prediction of wind-turbine fatigue loads in forest regions based on turbulent LES inflow fields, Volume 20, Issue 6 pp. 1003-1015, Wind Energy, 2017.
- L. Davidson, http://www.tfd.chalmers.se/~lada/projects/inlet-boundary-conditions/proright.html.